122
Compiled by Peter Schmidleitner
DA40 NG
243
Time, Fuel, Distance to Climb:
Based on ISA, zero wind
Add 5% to time and fuel,
10% to distance
for each 10
°
increase of OAT
Method of calculation:
1. get values for airfield altitude
2. get values for for cruise altitude
Result: subtract 1 from 2
243
Time, Fuel, Dist to climb
Compiled by Peter Schmidleitner
DA40 NG
244
Peter Schmidleitner
True Air Speed
Up to
16000 ft
Only one table for
1310kg